Contracting State
Civil Aviation Authority
Type Certificate No. ____
Pursuant to Civil Aviation Regulations Number ________of Contracting State, this Type
Certificate is issued to:
- Name of Holder of Type Certificate -
- Complete Address of Holder of Type Certificate -
For the following Aeronautical product(s):
-Aircraft Model __________ -
Details of this type design, basis of certification, operating limitations and other associated airworthiness requirements are specified in:
Civil Aviation Authority Type Certificate Data Sheet _____ or latest revision
Authorized Person – Civil Aviation Authority
Date of Issue
— — — — — — — —
APPENDIX B.— EXAMPLE OF A TYPE CERTIFICATE DATA SHEET
CIVIL AVIATION AUTHORITY CAA TYPE CERTIFICATE DATA SHEET CAA TCDS Code and Number Aircraft name Manufacturer: Manufacturer name and address For models: Aircraft name Issue 1, Draft 1: DD.MM.YY List of effective pages: All pages are at the latest issue
SECTION 1. GENERAL
.
Data Sheet No.: TCDS authority code and number
.
Airworthiness Category: Large airplane
y
Performance Category: A
y
Certifying Authority: Acronym
.
Type Certificate Holder: Name and address
.
ETOPS Not applicable
SECTION 2. AIRCRAFT NAME
2.I General
Aeroplane: ........................................................................................................... Aircraft Name
2.II FALCON 7X Certification Basis
.
Reference Application Date for EASA Certification: .......................................... DD.MM.YY
.
NAA Certification Date: ...................................................................................... DD.MM.YY
.
NAAA Certification Basis: ....................................................................................................
The following NAA airworthiness standards effective on the reference date are:
.
JAR 1 at change 5 plus orange papers 1/97/1 and 1/99/1
.
JAR 25 at change 15
.
JAR AWO at change 2
Refer to CRI A01 for exhaustive list of applicable requirements.
2. Requirements of JAR 25 change 15
Plus JAR 1 change 5 plus Orange papers 1/97/1 and 1/99/1.
Special Conditions:
CRI B-01 Stalling and scheduled operating speeds
CRI B-02 Motion and effects of cockpit controls
CRI B-03 Static directional, lateral and longitudinal stability and low energy
awareness
CRI B-04 Flight envelope protection
CRI B-05 Normal load factor limiting system
CRI C-01 Design maneuver requirements
CRI C-02 Limit forces and torque
CRI C-03 Design dive speed Vd
CRI C-05 Interaction of systems and structure
CRI C-06 Fuel tank crashworthiness
CRI D-02 Electronic flight control unusual features
CRI D-05 Flight controls - Harmonized 25.671
CRI D-07 Nose wheel steering - Towbarless towing
CRI D-09 Airworthiness standards for subsonic aeroplanes to be operated
above 41 000 ft
CRI D-11 Fire protection of thermal and acoustic insulation material
CRI D-22 Fuselage doors
CRI E-01 Fuel tank safety
CRI E-04 Reversing system requirements
CRI E-05 Sustained engine imbalance
CRI F-06 Protection from effects from HIRF
CRI F-24 Human factors aspects of flight deck design
CRI F-36 Head up display system
Exemptions: none
Deviation: CRI D-18 Personal injury criteria of dynamic testing of side facing sofa
Equivalent Safety Findings:
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